As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING EC/TC AD2004-10-030002 VISUAL INSP OF THE ENG SUPPORT BEAM, FOUND BOX BEAM UPPER WEB CRACKED UNDER THE BLEED AIR LEAK DETECTION BRACKET AT RBL9.5. AND AT FS640.00 CRACK MEASURES APPROX .375" PAST THE CLIP. CRACK HAS BEEN CONFIRMED BY METHOD OF EDDY CURRENT INSP.